Aerodynamic sound

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[B1-02] 高音圧が音響ライナ上の境界層に及ぼす影響

*Yuya Morii¹, Junichi Oki², Kei Wada², Tatsuya Ishii², Hitoshi Ishikawa³ (1. Department of Mechanical Engineering, Graduate School of Engineering, Tokyo University of Science Graduate School, 2. Japan Aerospace Exploration Agency, 3. Department of Mechanical Engineering, Faculty of Engineering, Tokyo University of Science)

Keywords:

Acoustic liner,Velocity distribution,Sound pressure,Boundary layer